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Target characteristic measurement system for drone aircraft

A technology for measuring system and target characteristics, applied in the field of unmanned aerial vehicle parameter measurement, can solve problems such as low positioning accuracy, inaccurate control of the flight attitude of the target aircraft, inaccurate measurement of flight parameters, etc., and achieve the effect of improving safety

Active Publication Date: 2016-01-13
BEIJING AEROSPACE KEYI TECH CO LTD +1
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem that the existing technology usually uses GPS positioning method to obtain the flight parameters of the target aircraft, the positioning accuracy of the system is not high, and the measurement of the flight parameters is not accurate. Therefore, this positioning method cannot be used as the main way to obtain the parameters of the unmanned aerial vehicle. The environment is relatively harsh, such as ducts, valleys, high mountains with bad weather, etc. In these areas, GPS or similar signals cannot be obtained, so this method of testing aircraft parameters is completely inapplicable. At the same time, in flight parameter measurement In the case of inaccuracy, the flight attitude of the target aircraft cannot be accurately controlled. The present invention provides a target characteristic measurement system for the target aircraft. The measurement system can not only accurately obtain the flight parameters of the target aircraft in real time, but also accurately control the The flight attitude of the target aircraft, so as to complete the flight mission of the ground server

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Embodiment 1

[0030] Such as figure 1 As shown, the embodiment of the present invention provides a system for measuring target characteristics of a target aircraft. The system includes an airborne flight control device, a flight parameter measurement device, and a ground transceiver control platform. The connection relationship can realize signal and data communication. The airborne flight control device communicates with the ground transceiver control platform. The communication connection is connected through a communication device. The communication device is a mechanical communication device, which includes Two structures of wireless reception and wireless transmission. The airborne flight control device receives the tasks sent by the ground transceiver control platform, and at the same time wirelessly sends the real flight parameters of the target aircraft to the ground transceiver control platform. Similarly, the ground communication equipment also has wireless reception. There are two ...

Embodiment 2

[0037] This embodiment 2 provides a target characteristic measurement system of a target aircraft, and this embodiment 2 further defines the inertial sensor, the flight parameter measurement device and the vibration amplitude sensor on the basis of embodiment 1, through the above-mentioned structure The limitation improves the accuracy of the measurement of the target characteristics of the target machine.

[0038] It should be noted that the inertial sensor includes an accelerometer and a gyroscope. The inertial sensor is a MEMS inertial sensor. The inertial sensor is an important part of navigation positioning, attitude measurement, orientation and motion carrier control. The inertial sensor mainly includes a gyroscope and an accelerometer. Inertial sensors have the characteristics of low cost, high reliability, small size, light weight, strong impact resistance, easy integration, mass production, low power consumption, and long life, and are practical. The inertial sensor...

Embodiment 3

[0042] The present embodiment 3 provides a kind of measuring system of target characteristics of target aircraft, and this embodiment 3 further limits the described measuring system on the basis of embodiment 1, and this measuring system further introduces the wind field measurement unit, by measuring the wind field The limitation of the unit ensures that the target aircraft can fly safely when it encounters a wind field during flight.

[0043] Such as Figure 7As shown, in order to enable the target drone to travel safely when encountering a wind field, the technical solution further defines that the measurement system also includes a wind field measurement unit arranged on the target drone, and the wind field measurement unit includes a horizontal ground speed measurement unit. Module, horizontal airspeed measurement module, wind field radar measurement module, signal amplification processing module and data calculation module, the output terminals of the horizontal ground s...

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Abstract

The invention relates to a target characteristic measurement system for a drone aircraft. The system comprises an airborne flight control device, a flight parameter measurement device and a ground transceiving control platform, wherein the flight parameter measurement device is connected with the airborne flight control device, and the airborne flight control device is in communication connection with the ground transceiving control platform. Through the airborne flight control device, the flight parameter measurement device and the ground transceiving control platform, the target characteristic measurement system for the drone aircraft can be used for measuring real flight parameters of the drone aircraft in real time and correcting and adjusting the real flight parameters, thus accurately measuring such real flight parameters of the drone aircraft as azimuth, pitching angle, flight height and the like; and through the real flight parameters, the accurate position of the drone aircraft can be determined, and the flight attitude of the drone aircraft can be effectively monitored, so that the safety is improved for the flight of the drone aircraft.

Description

technical field [0001] The invention relates to the field of parameter measurement of an unmanned aerial vehicle, in particular to a target characteristic measurement system of a target aircraft. Background technique [0002] At present, with the continuous improvement of the level of science and technology, the application of drones is becoming more and more extensive. With its good maneuverability and concealment, drones are becoming an indispensable weapon in modern high-tech warfare, and have been increasingly equipped with armies of various countries. In communication, meteorological monitoring, disaster monitoring, and geological survey, it can reduce labor intensity and reduce casualties. At the same time, the application of drones in civil fields such as surveying and mapping, aerial photography, and search is also expanding. [0003] The basic flight parameters of UAVs include attitude parameters, spatial position parameters, etc. These parameters are the premise a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08G01C21/00
Inventor 廖华龙
Owner BEIJING AEROSPACE KEYI TECH CO LTD